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具有CCV功能的直接力控制飞机,根据不同作战场合或完成某种特殊飞行功能的需要,飞行员按压所需的状态按钮,即可实现常规状态、直接升力、机身平移、机身俯仰、机动增强诸模态之间的转换。本文在微处理机单独实现各模态控制功能基础上,对各模态功能进行综合,指出模态转换的实现技术。本课题的混合仿真试验表明,各模态转换功能正常,模态转换瞬间飞机动态变化符合要求。本文为直接力控制技术的具体实施,或为一般的飞行控制状态切换提供一种可行的技术方案。
CCV-enabled direct-control aircraft, according to the needs of different combat situations or to complete a special flight function, the pilot presses the required state button, you can achieve the normal state, direct lift, fuselage pan, fuselage pitch, maneuver enhanced Conversion between modalities. Based on the realization of each modality control function by microprocessor alone, this paper summarizes the modal functions and points out the modal conversion technology. The mixed simulation experiments show that the modal conversion function is normal, and the dynamic changes of the aircraft meet the requirements at the moment of modal conversion. This article is the concrete implementation of the direct force control technology or provides a feasible technical solution for the general flight control state switching.